一种通用航空飞机半主动起落架控制的试验。
Test of Semiactive Landing Gear Control For a General Aviation Aircraft.
结合最优控制和自校正控制理论，给出了半主动起落架的自适应控制策略。
Combining optimal control and self-tuning control theory, the adaptive control strategy for semi-active landing gear is proposed.
介绍一种基于决策控制的半主动起落架减震器控制系统的动力学参数测量系统。
A dynamic parameter measurement system for absorber of undercarriage based on decision-making control is presented.
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